US9156208B2 - Infusion method and flow aid - Google Patents

Infusion method and flow aid Download PDF

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US9156208B2
US9156208B2 US13/519,935 US201013519935A US9156208B2 US 9156208 B2 US9156208 B2 US 9156208B2 US 201013519935 A US201013519935 A US 201013519935A US 9156208 B2 US9156208 B2 US 9156208B2
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component
flow
matrix material
body section
infusion method
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US20130099426A1 (en
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Clemens Heim
Paulin Fideu
Hauke Seegel
Axel Herrmann
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Airbus Operations GmbH
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Airbus Operations GmbH
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/02Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
    • B29C70/028Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers and with one or more layers of non-plastics material or non-specified material, e.g. supports
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/443Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/546Measures for feeding or distributing the matrix material in the reinforcing structure

Definitions

  • the invention concerns an infusion method for the manufacture of a fibre-reinforced composite.
  • FIGS. 1 to 3 A basic set-up for such infusion, or vacuum infusion, methods is shown in FIGS. 1 to 3 .
  • a component 2 composed of a base laminate 4 and an ancillary laminate 6 , which is to be infiltrated with a resin, is placed on a tool 8 and covered by a flow promoter 10 .
  • the laminates 4 , 6 consist of dry fibre-reinforced semi-finished products and are embodied as non-crimp fabrics (mats), knitted fabrics, woven fabrics, or similar.
  • the flow promoter 10 serves to provide an even distribution of the resin in the directions of the length and width of the component 2 and is, for example, a knit or a mesh of, for example, polyester or polyamide.
  • the component 2 and the flow promoter 18 are packaged in a vacuum bag (not shown), which is supported in a sealed manner on the tool 8 and which is evacuated via a suction device (not shown) close to the tool.
  • the resin is fed via a sprue (not shown) of the flow promoter that is remote from the tool.
  • the sprue is arranged in a left-hand region of the component, and the suction device in a right-hand region of the component.
  • a flow front 12 is formed, which impregnates the base laminate 4 in the thickness direction from left to right, wherein the resin in the vicinity of the flow promoter 10 runs ahead of the resin in the vicinity of the tool 8 somewhat, so that the flow front 12 is formed in the thickness direction at an inclined angle.
  • a component, i.e. laminate, thickness modification is present, which, as shown in FIG.
  • the object of the present invention is to create an infusion method and a flow promoter for the manufacture of a fibre-reinforced composite component that avoids the disadvantages cited above and enables an even and stable impregnation of the component fibres in the thickness direction.
  • a flow promoter for the distribution of a matrix material is placed on the composite component to be infiltrated.
  • the flow velocity of the matrix material within the flow promoter is modified in at least some sections, so that the whole infusion process is stabilised and the risk of porous inclusions is minimised or eliminated.
  • the propagation of the flow front can be specifically adjusted so that the above-described formation of a kink within the flow front can be controlled.
  • the flow velocity in the region of a thick-walled component section is slowed down.
  • the flow velocity can at least be slowed down so as to achieve a complete and stable impregnation of these component sections.
  • the flow velocity of the matrix material within the flow promoter is increased in some sections, so that, for example, the matrix material is guided faster across thin-walled component sections, since these can be more quickly impregnated in the thickness direction.
  • the flow velocity is preferably at least slowed down in the rear region of the thick-walled component region, i.e. near the transition, so that an even impregnation of the whole component section with the matrix material can be ensured.
  • the matrix material is temporarily halted in the flow promoter.
  • the flow promoter has a body section that serves as a kind of barrier for the matrix material and after a certain time is automatically dissolved by the matrix material.
  • the body section is dissolved by irradiation with an external energy source.
  • electromagnetic radiation such as UV-radiation, IR-radiation, and thermal radiation. That is to say, the body section is resistant to the matrix material.
  • This variant has the advantage that the dissolution of the body section does not have to be predetermined and thus the profile of the flow front can be specifically influenced in the course of the process in accordance with the set-up. Similarly by means of targeted irradiation only individual regions of the body section can be individually controlled. In this respect this example of embodiment allows for a certain tolerance in the design and positioning of the body section.
  • a further example of embodiment provides for the fact that the dissolution of the body section is initiated by irradiation with an external energy source and is then continued by the matrix material.
  • the start of the dissolution can be specifically determined and the dissolution per se can then proceed automatically.
  • An inventive flow promoter for an infusion method has at least one body section for purposes of modifying the flow velocity of the matrix material within the flow promoter.
  • the advantage of such a flow promoter consists in particular in the simple manipulation and positioning, and in the stabilisation of the whole process by minimisation of the risk of pore inclusions, independently of whichever infusion method is selected. A manual labour-intensive piecing together of the flow promoter and corresponding draping is avoided, so that complex components in particular can be manufactured more simply and more cost-effectively.
  • the body section is designed as a barrier that temporarily halts the matrix material. This temporary stop function can be achieved in that after a certain time the body section is dissolved, for example, by the matrix material.
  • the body section is formed from threads, which are manufactured, for example, from a plastic of the polyether sulphone group (PES).
  • PES polyether sulphone group
  • FIGS. 1 to 3 show a set-up and steps in the method for an infusion process of known art
  • FIGS. 4 to 8 show a set-up and steps in the method for an inventive infusion process.
  • a flow promoter 18 is used that has an integral body section 20 , which serves as a temporary barrier for a matrix material, e.g. a resin, flowing through the flow promoter 18 .
  • the base material of the flow promoter 18 is, for example, a polyester knitted fabric.
  • the body section 20 is formed from integral threads of, for example polyether sulphone (PES). These have the property that after a determinable and adjustable time they are dissolved by the adjacent resin, for example, an epoxy resin or a polyester resin of the RTM 6 class (see FIG. 8 ), so that the resin can propagate further within the flow promoter 18 unhindered.
  • the time after which the body section 20 dissolves is accurately determined in advance. In particular, this can be influenced by the number, thickness, and arrangement or alignment of the threads, materials and resin temperature.
  • inventive flow promoter 18 not only above a component 22 to be impregnated with the resin, but also underneath, i.e. between the component 22 and a tool surface 24 receiving the component 22 .
  • infusion techniques include resin transfer moulding (RTM), vacuum assisted process (VAP), vacuum resin infusion (VARI) and similar.
  • a component 22 to be impregnated with the resin is positioned on a tool surface 24 , as shown in FIG. 4 .
  • It has, for example, as a base laminate 4 at least one semi-finished textile product composed of dry fibres, and as an ancillary laminate 6 at least one second semi-finished textile product composed of dry fibres, which is placed centrally on the base laminate 4 .
  • the laminates 4 , 6 i.e. the semi-finished products, consist, for example, of carbon fibres or glass fibres, which are oriented to form a mat, a knitted fabric, a woven fabric, or similar.
  • the inventive flow promoter 18 is placed on the former so that the component 22 is arranged between the tool surface 24 and the flow promoter 18 .
  • the above-described arrangement is then packaged in a vacuum bag and evacuated, wherein, according to the arrow shown in FIG. 5 and indicating the flow direction of the resin, the introduction of the resin takes place in a left-hand region of the component, and removal by suction takes place in a right-hand region of the component.
  • the resin is then fed to the component 22 via the flow promoter 18 , wherein the component 22 is impregnated by the resin in the thickness direction and a flow front 26 propagates, which, in accordance with the flow direction of the resin in the flow promoter 18 , extends from left to right, here, that is to say, in the transverse direction, through the component 22 .
  • the resin in the region of the tool surface 24 is slightly held back relative to the resin in the region of the flow promoter 18 , so that the flow front 26 does not form parallel to the vertical axis of the component 22 but is oriented at a slight angle.
  • the resin distribution in the base laminate 6 remote from the flow promoter is further retarded, as shown in FIG. 6 , so that the flow front 26 is, so to speak, subdivided into two sections 28 , 30 that are separated from one another via a kink 14 , wherein the section 28 on the side of the base laminate propagates more slowly than the section 30 on the side of the ancillary laminate, so that the flow front 26 extends through the component 22 with quite different velocities.
  • the propagation of the ancillary laminate-side section 30 is slowed down in the transverse direction, and by this means the impregnation of the component 22 in the thickness direction is improved, as a result of which the propagation velocity of the base laminate-side section 28 is increased.
  • the barrier 20 is automatically dissolved by the resin that has already been present for some time and halted in the transverse direction, in accordance with FIG. 8 , so that a further distribution of the resin in the transverse direction of the component 22 through the base laminate 4 is possible, without the risk of porous areas ( FIG. 3 , 16 ) within the component 22 .
  • the component 22 is fully and evenly impregnated with the resin with the use of the inventive flow promoter 18 .

Abstract

Disclosed is an infusion method for the manufacture of a fiber-reinforced composite component with a flow promoter, wherein the flow velocity of the matrix material in a component to be infiltrated is modified by means of the flow promoter. Also disclosed is a flow promoter, which has an integral body section for the modification of the flow velocity.

Description

TECHNICAL FIELD
The invention concerns an infusion method for the manufacture of a fibre-reinforced composite.
BACKGROUND OF RELATED ART
A basic set-up for such infusion, or vacuum infusion, methods is shown in FIGS. 1 to 3. A component 2 composed of a base laminate 4 and an ancillary laminate 6, which is to be infiltrated with a resin, is placed on a tool 8 and covered by a flow promoter 10. The laminates 4, 6 consist of dry fibre-reinforced semi-finished products and are embodied as non-crimp fabrics (mats), knitted fabrics, woven fabrics, or similar. The flow promoter 10 serves to provide an even distribution of the resin in the directions of the length and width of the component 2 and is, for example, a knit or a mesh of, for example, polyester or polyamide. The component 2 and the flow promoter 18 are packaged in a vacuum bag (not shown), which is supported in a sealed manner on the tool 8 and which is evacuated via a suction device (not shown) close to the tool. The resin is fed via a sprue (not shown) of the flow promoter that is remote from the tool. In accordance with the resin flow direction indicated by the arrow the sprue is arranged in a left-hand region of the component, and the suction device in a right-hand region of the component.
With the feed of the resin a flow front 12 is formed, which impregnates the base laminate 4 in the thickness direction from left to right, wherein the resin in the vicinity of the flow promoter 10 runs ahead of the resin in the vicinity of the tool 8 somewhat, so that the flow front 12 is formed in the thickness direction at an inclined angle. In the vicinity of the ancillary laminate 6 a component, i.e. laminate, thickness modification is present, which, as shown in FIG. 2, leads to the fact that the resin is no longer stably distributed across the whole cross-section of the component 2, but is more severely retarded in the base laminate 4 remote from the flow promoter than in the ancillary laminate 6 close to the flow promoter, so that a kink 14 is formed, so to speak, in the flow front 12. As a result the risk exists that after the impregnation of the ancillary laminate 6 a porous area 16 may form in the base laminate 4 underneath the flow front 12, as shown in FIG. 3, which would significantly reduce the quality of the fibre composite component 2 to be manufactured.
In addition to the use of separate flow promoters, which are placed on the semi-finished product, i.e. on the component, it is likewise of known art from the applicant's application in DE 10 2007 013 987 A1 to integrate the flow promoter into the tool surface. However, even with this solution an even, stable distribution of the resin that is independent of the cross-section, i.e. the thickness, of the semi-finished product, cannot be reliably guaranteed.
SUMMARY
The object of the present invention is to create an infusion method and a flow promoter for the manufacture of a fibre-reinforced composite component that avoids the disadvantages cited above and enables an even and stable impregnation of the component fibres in the thickness direction.
This object is achieved by means of an infusion method with the features of claim 1.
In an inventive infusion method for the manufacture of a fibre-reinforced composite component a flow promoter for the distribution of a matrix material is placed on the composite component to be infiltrated. In accordance with the invention the flow velocity of the matrix material within the flow promoter is modified in at least some sections, so that the whole infusion process is stabilised and the risk of porous inclusions is minimised or eliminated. The propagation of the flow front can be specifically adjusted so that the above-described formation of a kink within the flow front can be controlled.
In one preferred example of embodiment the flow velocity in the region of a thick-walled component section is slowed down. By this means it is possible to achieve an even resin distribution across the whole thickness of the component, since the matrix material is guided across the component surface with at least a reduced velocity. Similarly in the case of complex component structures or sections the flow velocity can at least be slowed down so as to achieve a complete and stable impregnation of these component sections. In another example of embodiment the flow velocity of the matrix material within the flow promoter is increased in some sections, so that, for example, the matrix material is guided faster across thin-walled component sections, since these can be more quickly impregnated in the thickness direction.
In transitions from thick-walled to thin-walled component sections the flow velocity is preferably at least slowed down in the rear region of the thick-walled component region, i.e. near the transition, so that an even impregnation of the whole component section with the matrix material can be ensured.
In particular it is advantageous if the matrix material is temporarily halted in the flow promoter. By this means it is achieved that impregnation only in the thickness direction is possible for a certain period of time, and that the matrix material is only guided further across the component when the latter has been impregnated in the thickness direction to a particular extent. Here the set-up of the infusion method can be simplified if the flow promoter has a body section that serves as a kind of barrier for the matrix material and after a certain time is automatically dissolved by the matrix material.
In another form of embodiment the body section is dissolved by irradiation with an external energy source. Examples are electromagnetic radiation such as UV-radiation, IR-radiation, and thermal radiation. That is to say, the body section is resistant to the matrix material. This variant has the advantage that the dissolution of the body section does not have to be predetermined and thus the profile of the flow front can be specifically influenced in the course of the process in accordance with the set-up. Similarly by means of targeted irradiation only individual regions of the body section can be individually controlled. In this respect this example of embodiment allows for a certain tolerance in the design and positioning of the body section.
A further example of embodiment provides for the fact that the dissolution of the body section is initiated by irradiation with an external energy source and is then continued by the matrix material. By this means the start of the dissolution can be specifically determined and the dissolution per se can then proceed automatically.
An inventive flow promoter for an infusion method has at least one body section for purposes of modifying the flow velocity of the matrix material within the flow promoter. The advantage of such a flow promoter consists in particular in the simple manipulation and positioning, and in the stabilisation of the whole process by minimisation of the risk of pore inclusions, independently of whichever infusion method is selected. A manual labour-intensive piecing together of the flow promoter and corresponding draping is avoided, so that complex components in particular can be manufactured more simply and more cost-effectively.
In one preferred example of embodiment the body section is designed as a barrier that temporarily halts the matrix material. This temporary stop function can be achieved in that after a certain time the body section is dissolved, for example, by the matrix material.
In one variant the body section is formed from threads, which are manufactured, for example, from a plastic of the polyether sulphone group (PES).
Other advantageous examples of embodiment of the present invention are the subject of further dependent claims.
BRIEF DESCRIPTION OF THE DRAWINGS
In what follows preferred examples of embodiment of the invention are elucidated in more detail with the aid of schematic representations. Here:
FIGS. 1 to 3 show a set-up and steps in the method for an infusion process of known art; and
FIGS. 4 to 8 show a set-up and steps in the method for an inventive infusion process.
DETAILED DESCRIPTION
In a preferred infusion process in accordance with FIG. 4, a flow promoter 18 is used that has an integral body section 20, which serves as a temporary barrier for a matrix material, e.g. a resin, flowing through the flow promoter 18. The base material of the flow promoter 18 is, for example, a polyester knitted fabric. In contrast, the body section 20 is formed from integral threads of, for example polyether sulphone (PES). These have the property that after a determinable and adjustable time they are dissolved by the adjacent resin, for example, an epoxy resin or a polyester resin of the RTM 6 class (see FIG. 8), so that the resin can propagate further within the flow promoter 18 unhindered. The time after which the body section 20 dissolves is accurately determined in advance. In particular, this can be influenced by the number, thickness, and arrangement or alignment of the threads, materials and resin temperature.
In what follows an infusion method using the inventive flow promoter 18 is elucidated: Here, however, reference is only made to the significant features, and aspects of general known art concerning the set-up of an infusion method are not elucidated in any further detail. Thus, for example, peel plies, vacuum bags, positioning of the sprue and/or suction device, and ventilation weaves, are not shown, and some are even not further mentioned. This, however, does not mean that the inventive flow promoter 18 can only be deployed in the set-up here described. The aspects or features of a set-up for an infusion method that are not further mentioned are, however, items that are obvious. Similarly it is an obvious matter to arrange the inventive flow promoter 18 not only above a component 22 to be impregnated with the resin, but also underneath, i.e. between the component 22 and a tool surface 24 receiving the component 22. Examples of infusion techniques include resin transfer moulding (RTM), vacuum assisted process (VAP), vacuum resin infusion (VARI) and similar.
At the start of the infusion method, a component 22 to be impregnated with the resin is positioned on a tool surface 24, as shown in FIG. 4. It has, for example, as a base laminate 4 at least one semi-finished textile product composed of dry fibres, and as an ancillary laminate 6 at least one second semi-finished textile product composed of dry fibres, which is placed centrally on the base laminate 4. The laminates 4, 6, i.e. the semi-finished products, consist, for example, of carbon fibres or glass fibres, which are oriented to form a mat, a knitted fabric, a woven fabric, or similar.
After the positioning of the component 22 on the tool surface 24 the inventive flow promoter 18 is placed on the former so that the component 22 is arranged between the tool surface 24 and the flow promoter 18.
The above-described arrangement is then packaged in a vacuum bag and evacuated, wherein, according to the arrow shown in FIG. 5 and indicating the flow direction of the resin, the introduction of the resin takes place in a left-hand region of the component, and removal by suction takes place in a right-hand region of the component. The resin is then fed to the component 22 via the flow promoter 18, wherein the component 22 is impregnated by the resin in the thickness direction and a flow front 26 propagates, which, in accordance with the flow direction of the resin in the flow promoter 18, extends from left to right, here, that is to say, in the transverse direction, through the component 22. By virtue of the resin feed via the flow promoter 18 the resin in the region of the tool surface 24 is slightly held back relative to the resin in the region of the flow promoter 18, so that the flow front 26 does not form parallel to the vertical axis of the component 22 but is oriented at a slight angle.
As soon as the resin is fed via the flow promoter 18 into the region of the ancillary laminate, or the local reinforcement layers 6, the resin distribution in the base laminate 6 remote from the flow promoter is further retarded, as shown in FIG. 6, so that the flow front 26 is, so to speak, subdivided into two sections 28, 30 that are separated from one another via a kink 14, wherein the section 28 on the side of the base laminate propagates more slowly than the section 30 on the side of the ancillary laminate, so that the flow front 26 extends through the component 22 with quite different velocities.
However, if the matrix material within the flow promoter 18 runs onto the body section 20 arranged in the rear region near a transition to the base laminate 4, as shown in FIG. 7, the propagation of the ancillary laminate-side section 30 is slowed down in the transverse direction, and by this means the impregnation of the component 22 in the thickness direction is improved, as a result of which the propagation velocity of the base laminate-side section 28 is increased.
As soon as a sufficient harmonisation of the two flow front sections 28, 30 is achieved, for example by a flattening out, or an approximate flattening out, of the kink 14, the barrier 20 is automatically dissolved by the resin that has already been present for some time and halted in the transverse direction, in accordance with FIG. 8, so that a further distribution of the resin in the transverse direction of the component 22 through the base laminate 4 is possible, without the risk of porous areas (FIG. 3, 16) within the component 22. In this manner the component 22 is fully and evenly impregnated with the resin with the use of the inventive flow promoter 18.
Disclosed is an infusion method for the manufacture of a fibre-reinforced composite component with a flow promoter 18, wherein the flow velocity of the matrix material in a component 22 to be infiltrated is modified by means of the flow promoter 18; also disclosed is a flow promoter 18, which has an integral body section 20 for the modification of the flow velocity.
REFERENCE SYMBOL LIST
  • 2 Component
  • 4 Base laminate
  • 6 Ancillary laminate
  • 8 Tool
  • 10 Flow promoter
  • 12 Flow front
  • 14 Kink
  • 16 Porous area
  • 18 Flow promoter
  • 20 Body section
  • 22 Component
  • 24 Tool surface
  • 26 Flow front
  • 28 Section
  • 30 Section

Claims (7)

What is claimed is:
1. An infusion method for the manufacture of a fiber-reinforced composite, comprising:
covering a fiber-reinforced component with a flow promoter and providing said flow promoter with a body section for modifying a flow velocity of a matrix material used to impregnate the component, the body section integral with the flow promoter and formed from threads of a dissolvable material;
introducing the matrix material from an injection region;
distributing the matrix material in a thickness direction across the component, wherein the flow velocity of the matrix material is modified in the thickness direction through the component in a rear region of a thick-walled component section opposite to the injection region; and
dissolving the threads of the body section after a harmonization of different flow velocities through the component.
2. The infusion method in accordance with claim 1, further comprising slowing down the flow velocity in the rear region of the thick-walled component section opposite to the injection region.
3. The infusion method in accordance with claim 1, further comprising halting the matrix material temporarily in the flow promoter.
4. The infusion method in accordance with claim 1, wherein the body section is dissolved by the matrix material.
5. The infusion method in accordance with claim 1, wherein the body section is dissolved by irradiation.
6. The infusion method in accordance with claim 1, wherein the dissolution of the body section is initiated by irradiation and is then continued by the matrix material.
7. The infusion method in accordance with claim 1, wherein the body section is provided in a region of the flow promoter opposite to the injection region in the transverse direction.
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US13/519,935 US9156208B2 (en) 2009-12-29 2010-12-29 Infusion method and flow aid
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DE102014017809B4 (en) 2014-12-03 2017-03-23 Audi Ag Process for producing a structural component
DE102014118670B4 (en) * 2014-12-15 2016-06-30 Benteler Sgl Gmbh & Co. Kg RTM method with intermediate fiber layer
DE102015005492B4 (en) 2015-04-30 2023-05-04 Airbus Defence and Space GmbH Flow aid for an infusion structure and infusion structure and method for infiltrating a fibrous material
CN109070500B (en) 2016-03-25 2021-04-20 肖特兄弟公司 Apparatus and method for making composite laminates
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DE102009060699A1 (en) 2011-06-30
US20130099426A1 (en) 2013-04-25
WO2011080288A1 (en) 2011-07-07
EP2519401A1 (en) 2012-11-07

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